Maximum Vortex-Induced Side Force-Reference-Cited by-同舟云学术

Maximum Vortex-Induced Side Force

Published:1978-07 Issue:4 Volume:15 Page:201-207
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Reding J. Peter¹,Ericsson Lars E.¹

Affiliation:

1. Lockheed Missiles & Space Co., Inc., Sunnyvale, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.57306

Reference47 articles.

1. The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidence

2. Asymmetric Vortex Effects on Missile Configurations

3. 3Chambers, J. P., Anglin, E. L., and Bowman, J. B. Jr. "Effects of Pointed Nose on Spin Characteristics of a Fighter Airplane Model Including Correlation with Theoretical Calculations," NASA TN D5921,1970.

4. Investigation of side forces on ogive-cylinder bodies at high anglesof attack in the M equals 0.5 to 1.1 range

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